AD 95-11-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | ATR - GIE Avions de Transport Régional | ATR42-200 | Airworthiness Directives; Aerospatiale Model ATR42-200, -300, and -320 Series Airplanes |
| aircraft | ATR - GIE Avions de Transport Régional | ATR42-300 | Airworthiness Directives; Aerospatiale Model ATR42-200, -300, and -320 Series Airplanes |
| aircraft | ATR - GIE Avions de Transport Régional | ATR42-320 | Airworthiness Directives; Aerospatiale Model ATR42-200, -300, and -320 Series Airplanes |
Unsafe Condition
Loss of a propeller and engine gearbox resulting in fuselage damage could sever the elevator flight controls, leading to reduced controllability of the airplane.
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Required Actions
Modify the wiring in the elevator controls and pitch trim dissymmetry monitoring equipment in accordance with Aerospatiale Service Bulletins ATR42-27-0068 or ATR42-27-0069, dated January 25, 1994.
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Compliance Time
Within 12 months after the effective date of this AD
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Affected Aircraft
Aerospatiale Model ATR42-200, -300, and -320 series airplanes as listed in Service Bulletins ATR42-27-0068 and ATR42-27-0069, dated January 25, 1994; certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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